Four-rotor aircraft formation tracking control method
A quadrotor aircraft, tracking control technology, applied in attitude control, adaptive control, electric controller and other directions, can solve the problems of convergence time effect, complex dynamics, unmanned aerial vehicle can not fly, etc., to achieve strong robustness and stability. Noise immunity, fixed time convergence, effect of reducing coupling
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[0047] Such as figure 1 As shown, the multi-UAV formation control method based on the fixed time consistency theory proposed by the present invention, the specific implementation is as follows:
[0048] Take 3 drones and a virtual leader as an example, set the total flight time to 15 seconds, and observe whether the drones form the desired formation and the formation time.
[0049] Step 1: Give the quadrotor drone a dynamic model, the specific steps are as follows:
[0050] The four inputs of the UAV are generated by the four rotors, and the four rotor pulls and three axial moments are obtained. The resultant pull of the four rotors is T i , the torque is τ φ,i is the rolling moment, τ θ,i is the pitching moment, τ ψ,i is the yaw moment, and the moment imbalance is the reason for the rotational motion of the UAV. If the rotational speeds of the four rotors are respectively w 1,i ,w 2,i ,w 3,i ,w 4,i ,Available
[0051]
[0052] where b is 10Nms 2 In order to re...
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